A non-gaussian atmospheric turbulence model for flight simulator studies of aircraft handling qualities / by C.J. JansenA method of characteristic surfaces : the approximate solution of three-dimensional supersonic flow fields, from the near field up to the sonic boom region / Th.P.M. HendriksIntegral equation methods for multi-element airfoil analysis and design / by Th.E. LabrujèrePatch repair of corroded aircraft skin areas / W.G.J. 't Hart, R.J.H. WanhillProblem and solution formulations for the generation of 3D block-structured grids / by J.W. BoerstoelThe use of standarized fatigue load sequences in coupon and component tests / by J.B. de JongeBreukmechanica en kruipscheurgroei in staal van het type 1%Cr1/2%Mo al dan niet na voorafgaande expositie onder kruipomstandigheden / door H.P. van Leeuwen en L. SchraFatigue fracture in landing gear steels / by R.J.H. WanhillCalculation of 2-D unsteady transonic full potential flow about oscillating airfoils by two complementary approaches / by H. Schippers and M.H.L. HounjetEvaluation of Ting's method for the calculation of the lift distribution on a wing in propulsive jets / by R.A. MaarsinghData acquisition and analysis system as a training device for simulated convential weapon delivery / by C.F.G.M. Hofman and J. BatenburgA wind-tunnel study of the flutter characteristics of a supercritical wing / by R. Houwink, A.N. Kraan and R.J. ZwaanSome remarks on boundary layer effects on unsteady airloads / by R. HouwinkEffects of variations in gust spectrum and ground load level on fatigue life and crack propagation / by A. Nederveen, J.B. de Jonge and P.J. TrompOntwerp van een vaste brandstof verbrandingskamer / P.A.O.G. KortingVerification of obstacle accountability areas using a simple mathematical model / G. MoekARSNPS: a method to calculate steady and unsteady potential flow about fixed and rotating lifting and nonlifting bodies / by M.H.L. HounjetUnconventional aircraft concepts : papers presented at a symposium organized by The Netherlands Association of Aeronautical Engineers (NVvL) and the Students Society 'Leonardo da Vinci' on april 24, 1987, at the Delft University of Technology / F.J. Sterk, F.J. Sterk (eds.)Focus / publ. by Fokker-VFW InternationalA method for measuring take-off and landing performance of aircraft, using an inertial sensing system / by A. Pool ... [et al.]A calculation method for the viscous flow around multi-component airfoils / by B. OskamComputational aspects and results of low-speed viscous flow about multicomponent airfoils / by B. OskamVerslag van de werkzaamheden / Nederlands Instituut voor Vliegtuigontwikkeling en RuimtevaartTransmission of sinussoidally changing vertical specific force to the heads of seated men measured in a flight simulator / by R.A.A. Reutlinger and J.C. van der VaartOn the acoustical implications of vortex shedding from an exhaust pipe / by S.W. RienstraSound diffraction at a trailing edge / S.W. RienstraThe international vortex flow experiment : a test case for compressible Euler codes / by A. ElsenaarTests on the AFWAL 65° delta wing at NLR : a study of vertex flow development between Mach = 0.4 and 4 / by S.J. Boersen and A. ElsenaarThree-dimensional shear layer experiments and their use as test cases for caluculation methods / by B. van den BergNLR contributions to the flutter certification of aircraft with external stores / by J.J. MeijerTheoretical and experimental investigations into vortex flow / by H.W.M. Hoeijmakers and N.G. VerhaagenDetermination of low-speed longitudinal manoeuvring criteria for transport aircraft with advanced flight control systems / by H.A. Mooij, W.P. de Boer and M.F.C. van GoolFlying qualities criteria for advanced control technology transport / by H.A. MooijShear layer effects on pure tone sound propagation in open jet wind tunnels using 1/3 octave analysis / by R. RossAn approximate method for computing inviscid vortex wake roll-up / H.W.M. HoeijmakersFracture mechanics and creep crack growth of 1%Cr1/2%Mo steel with and without prior exposure to creep conditions / by H.P. van Leeuwen and L. SchraJaarboek / Vliegtuigbouwkundige Studievereniging "Leonardo da Vinci"Fracture characteristics of carbon and aramid unidirectional composites in interlaminar shear and open hole tensile tests / by A.C. Moss and W.G.J. 't HartTrends in CFD for aeronautical 3-D steady applications : the Dutch situation / by J.W. Boerstoel ... [et al.]The initial calculation of range and mission fuel during conceptual design / E. Torenbeek